Hinge assembly for deploying the petals of a sectored mirror of an optical space telescope

• US 6,956,696 B2
• Filed: 11/16/2004
• Issued: 10/18/2005
• Est. Priority Date: 08/09/2002
• Status: Expired due to Fees

• Current Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Hachkowski, M. Roman, Cox, Charles D.
• Primary Examiner(s): Robinson, Mark A.
• Application Number:
  US10/990,240
• Publication Number:
  US 20050094264A1
• Time in Patent Office: 336 Days
• Field of Search: 359/399, 244/158.R, 244/173, 248/346.3, 248/472, 162/73, 162/76
• US Class Current: 359/399
• CPC Class Codes: B64G 1/222 for deploying structures between a stowed and deployed state
• CPC Class Codes: B64G 1/641 Interstage or payload connectors docking systems B64G1/646
• CPC Class Codes: B64G 1/66 Arrangements or adaptations of apparatus or instruments, not otherwise provided for
• CPC Class Codes: F16C 2326/47 Cosmonautic vehicles, i.e. bearings adapted for use in outer-space in general B64G
• CPC Class Codes: F16C 31/04 Ball or roller bearings
• CPC Class Codes: F16C 33/32 Balls
• CPC Class Codes: F16C 33/40 for multiple rows of balls
• CPC Class Codes: F16C 33/56 Selection of substances F16C33/48, F16C33/49 take precedence
• CPC Class Codes: G02B 7/183 specially adapted for very large mirrors, e.g. for astronomy, or solar concentrators

Abstract

A system is disclosed for deploying the petals of a sectored mirror assembly of an optical space telescope, wherein the sectored mirror includes a central hub and a plurality of petals disposed about the periphery of the central hub, and each petal has a petal root independently hinged to the central hub. The system includes a first hinge assembly having a root mount secured to a petal root and a hub mount secured the central hub, whereby the first hinge assembly affords the petal associated therewith freedom of rotation about a petal hinge axis. The system further includes a second hinge assembly including a root mount secured to the petal root and a hub mount secured to the central hub, whereby the second hinge assembly affords the petal associated therewith freedom of rotation about the petal hinge axis and freedom to expand and contract thermally, and move rigidly along the petal hinge axis in a frictionless, unconstrained manner. The system also includes a latch assembly including a clevis secured to the petal root at a location spaced from the hinge axis and a pair of laterally opposed latch mechanism operatively associated with the central hub for engaging the clevis upon rotation of the petal about the hinge axis from a stowed position to a deployed position.

Claims

1. A petal deployment hinge assembly for connecting a petal of a sectored mirror of an optical space telescope to the central hub of the sectored mirror, the hinge assembly comprising:

a) a root mount secured to a root of the petal;

b) a hub mount secured to the central hub;

c) an axial hinge shaft supported by the root mount; and

d) a cylindrical bearing cage disposed about the hinge shaft and housed within the hub mount for affording rotational and axial movement of the root mount relative to the hub mount along the axis of the hinge shaft.

2. A petal deployment hinge assembly as recited in claim 1, wherein the bearing cage is formed from PTFE.

3. A petal deployment hinge assembly as recited in claim 1, wherein the bearing cage retains a plurality of ball bearings.

4. A petal deployment hinge assembly as recited in claim 3, wherein the ball bearings are formed from silicon nitride.

5. A petal deployment hinge assembly as recited in claim 4, wherein the bearing cage is disposed between an inner bearing race and an outer bearing race.